A stabilization system and method for an unmanned aerial vehicle (UAV) (fig 1, 100) carrying a payload 2414. A housing body houses control circuitry of the UAV. One or more rotors 2402, 2404, 2406, 2408 are arranged around the housing body 2410 to power flight of the UAV. One or more sliding guides are provided at the housing body. A movable attachment point (fig 29, 2908) is slidably connected to the sliding guide(s) (fig 29, 2805) of the housing body. One or more sensors are capable of sensing displacement of the movable attachment point and generating a signal relating to the displacement and to transmit it to the control circuitry. The control circuitry is arranged, in response to receiving the signal relating 0 to the displacement, to analyse the signal and to output a control signal for adjusting rotor speeds 1 of one or more of the rotors so as to stabilize a payload carried by the UAV. The housing body may include two sliding guides crossing one another and that intersect at a central region of the housing body. The sliding guides may be perpendicular to one another. A corresponding method is also disclosed.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Control system for UAVS


    Erscheinungsdatum :

    06.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Control system for uavs

    Europäisches Patentamt | 2024

    Freier Zugriff

    Control system for UAVs

    STEPHEN LARKIN / MUHAMMAD OMAR / AATIF ALI et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Trinocular ground system to control UAVs

    Martinez, Carol / Campoy, Pascual / Mondragon, Ivan et al. | Tema Archiv | 2009


    UAVs and Control Delays

    S. C. de Vries | NTIS | 2005


    Control of Micro-UAVs

    Amitay, Michael | AIAA | 2010